DocumentCode :
3204398
Title :
On information measures based on particle mixture for optimal bearings-only tracking
Author :
Skoglar, Per ; Orguner, Umut ; Gustafsson, Fredrik
Author_Institution :
Dept. of Electr. Eng., Linkoping Univ., Linkoping
fYear :
2009
fDate :
7-14 March 2009
Firstpage :
1
Lastpage :
14
Abstract :
In this work we consider a target tracking scenario where a moving observer with a bearings-only sensor is tracking a target. The tracking performance is highly dependent on the trajectory of the sensor platform, and the problem is to determine how it should maneuver for optimal tracking performance. The problem is considered as a stochastic optimal control problem and two sub-optimal control strategies are presented based on the Information filter and the determinant of the information matrix as the optimization objective. Using the determinant of the information matrix as an objective function in the planning problem is equivalent to using differential entropy of the posterior target density when it is Gaussian. For the non-Gaussian case, an approximation of the differential entropy of a density represented by a particle mixture is proposed. Furthermore, a gradient approximation of the differential entropy is derived and used in a stochastic gradient search algorithm applied to the planning problem.
Keywords :
approximation theory; optimal control; position control; search problems; stochastic systems; target tracking; differential entropy; information matrix; optimal bearings-only tracking; particle mixture; stochastic gradient search algorithm; stochastic optimal control problem; suboptimal control strategies; target tracking; Dynamic programming; Entropy; Information filters; Mutual information; Optimal control; Particle measurements; Particle tracking; Stochastic processes; Target tracking; Trajectory;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace conference, 2009 IEEE
Conference_Location :
Big Sky, MT
Print_ISBN :
978-1-4244-2621-8
Electronic_ISBN :
978-1-4244-2622-5
Type :
conf
DOI :
10.1109/AERO.2009.4839487
Filename :
4839487
Link To Document :
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